Burning surfaces evolution in solid propellants: a numerical model

A methodology for the solution of the internal physics of solid propellant rocket motors is described. The problem involves the simulation of a burning surface - a dynamically changing interface between the solid propellant and combustion gas phases. Burning surfaces can have complex shapes that cha...

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Bibliographic Details
Main Authors: Joanna Szmelter, P. Ortiz
Format: Default Article
Published: 2007
Subjects:
Online Access:https://hdl.handle.net/2134/4693
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